摘要
应用20kHz超声疲劳试验系统和高频疲劳试验系统,对TC32钛合金材料室温对称载荷作用下的超高周疲劳进行了研究。结果表明:疲劳循环在10~7周次后仍会发生断裂,不存在明显的疲劳极限,S-N曲线呈现双线性特征;从疲劳断口特征来看,较高应力下为表面萌生机制,而在低应力超高周疲劳范围内,裂纹则主要于亚表面萌生;加载频率对TC32钛合金疲劳行为无明显影响。
The ultra-high cycle fatigue performance and failure mechanism of TC32 titanium alloy under the action of room temperature and symmetric load were studied by 20 kHz ultrasonic fatigue test system. The result shows that break will still arise after 10~7 cycles, there is no obvious fatigue limit, the SN curve exhibits bilinear characteristics;At higher stress, the surface initiation mechanism is exhibited, while in the low stress and high cycle fatigue range, the crack is mainly caused at subsurface;the loading frequency has no significant effect on the fatigue behavior of TC32 alloy.
作者
王泽民
王晓瑞
孟扬
郑逸超
赵子华
Wang Zemin;Wang Xiaorui;Meng Yang;Zheng Yichao;Zhao Zihua(School of Materials Science and Engineering,Beihang University,Beijing 100191,China;Centre de Thermique de Lyon(CETHIL)UMR5008,Universitéde Lyon,INSA de Lyon,CNRS,UniversitéLyon 1,Lyon F-69621,France;School of Energy and Power Engineering,Beihang University,Beijing 100191,China)
出处
《金属热处理》
CAS
CSCD
北大核心
2019年第S01期595-598,共4页
Heat Treatment of Metals
关键词
TC32钛合金
超高周疲劳
S-N曲线
组织
TC32 titanium alloy
ultra-high cycle fatigue
S-N curve
microstructure